3-DIMENSIONAL FLOW FIELD IN ROCKET PUMP INDUCERS .1. MEASURED FLOW FIELD INSIDE ROTATING BLADE PASSAGE AND AT EXIT

被引：5

作者：

LAKSHMINARAYANA, B ^{[1
]}

机构：

[1] PENN STATE UNIV, UNIVERSITY PK, PA 16802 USA

来源：

JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME | 1973年 / 95卷 / 04期

关键词：

D O I：

10.1115/1.3447071

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：567 / 578

页数：12

共 9 条

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GRACEY W, 1957, NACA1303 REP

[2] TURBULENT BOUNDARY-LAYER ON A ROTATING HELICAL BLADE [J].

LAKSHMINARAYANA, B ;

YAMAOKA, H ;

JABBARI, A .

[3]

LAKSHMINARAYANA B, SP304 NASA

[4]

LAKSHMINARAYANA B, ASME73FE31 PAP

[5]

LAKSHMINARAYANA B, 1972, T ASME D, V94

[6]

LAKSHMINARAYANA B, 1972, 2 P INT JSME S, V1, P157

[7]

MCCAFFERTY HG, 1967, THESIS PENNSYLVANIA

[8]

PONCET A, 1973, CR2290 NASA

[9]

Schlichting H., 1961, BOUNDARY LAYER THEOR, V9th ed.